Research on High-Angle Tracking Method of Forward and Backward Mirror Program Guidance by Azimuth-Pitching Antenna

Fei Gao, Zhuo Zhang, Zongqing Wu, Guohua Zhao, Min Liang, Yijia Li
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Abstract

There is a certain tracking blind area near the zenith when azimuth-pitching antenna is tracking, and the program guidance mode is usually used to complete the high-angle tracking. In this way, the target will be lost for a period of time and the efficiency of antenna equipment will be affected. This paper proposed a high-angle tracking method of forward and backward mirror program guidance based on the driving performance of antenna, and makes a quantitative analysis for the two kinds of program from the aspects of overheard time, pointing error and azimuth maximum velocity. It not only solves the smooth angles transition of the antenna near the zenith and the closed-loop switching stability of tracking mode, it can make up for the deficiency that the current program guidance cannot give full play to the antenna performance when go over the top, and minimize the antenna overheard time and the pointing error correspondingly, so as to minimize the antenna overhead blind area and improve utilization rate of the antenna.
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方位角-俯仰天线前后镜程序制导的大角度跟踪方法研究
方位角俯仰天线进行跟踪时,在天顶附近存在一定的跟踪盲区,通常采用程序制导方式完成大角度跟踪。这样会使目标丢失一段时间,影响天线设备的工作效率。本文提出了一种基于天线驱动性能的正反镜程序制导的高角度跟踪方法,并从窃听时间、指向误差和方位角最大速度三个方面对两种程序进行了定量分析。它不仅解决了天线在天顶附近角度的平滑过渡和跟踪方式的闭环切换稳定性,还可以弥补当前节目制导在超过天顶时不能充分发挥天线性能的不足,并相应最小化天线窃听时间和指向误差,从而最大限度地减小天线顶置盲区,提高天线的利用率。
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